EVALUATION OF AN AUTOMATIC INLET-PRESSURE CONTROL VALVE FOR STUDY OF TRANSIENT ENGINE PERFORMANCE CHARACTERISTICS. PDF Download
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Category :
Languages : en
Pages : 28
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Author:
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Category :
Languages : en
Pages : 28
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Author: United States. National Advisory Committee for Aeronautics
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Category : Aeronautics
Languages : en
Pages : 382
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Author: United States. National Advisory Committee for Aeronautics
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Category : Aeronautics
Languages : en
Pages : 716
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Author:
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Category : Aeronautics
Languages : en
Pages : 388
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Author:
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Category : Aeronautics
Languages : en
Pages : 456
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Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
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Languages : en
Pages : 600
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Author: John R. Szuch
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Category : Airplanes
Languages : en
Pages : 52
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The analysis of data obtained from sweep-frequency testing of the 585 turbojet combustor is discussed.Bode plots of the response of combustor pressure to sinusoidal disturbances in fuelspray- nozzle pressure are presented for a range of fuel flows. An analog simulation was developed and used to match the experimental data and to identify the combustion dynamics. The effects of primary or burning-zone fuel-to-air ratio on the system response were also investigated. The experimental data were fit by linear transfer function forms to be used in overall system studies.
![Cumulative Index [of The] SAE Papers PDF](https://books.google.com/books/content/images/frontcover/mmIcAQAAMAAJ?fife=w80-h100)
Author: Society of Automotive Engineers
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Category : Engineering
Languages : en
Pages : 1646
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Category : Electrical engineering
Languages : en
Pages : 320
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Author:
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Category : Electrical engineering
Languages : en
Pages : 698
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